# Service difficulty reports: N368NB

A list on [N368NB](https://openairdocs.org/aircraft/N368NB.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 107 reports

- [SDR DALA2026052803231](https://openairdocs.org/sdr/DALA2026052803231.md): Window Frame · broken · May 27, 2026 · N368NB · Airbus A319114 · Fuselage Main, Structure
  > DURING THE M2 CHECK (D CHECK) AT COO (SJO), AND WHILE EXECUTING A DELTA TASK CARD INSTRUCTIONS RELATED TO SB A320-53-1331 R01 AND AD 2020-17-03, THE LT CONTINUITY FITTING AND WINDSHIELD FRAMING WITH CRACK WERE FOUND. CORRECTIVE ACTION: PERFORMED WINDSHIELD FRA
- [SDR DALA2026052703186](https://openairdocs.org/sdr/DALA2026052703186.md): Floor Support · corroded · May 26, 2026 · N368NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3168 DISC: LEVEL 2 CORROSION, TASK 5310-3040, CORROSION SSI: 531189, CPCP TASK 2021-2001. FWD PASSENGER CABIN BETWEEN FR 16-20, Y 254, FLOOR BEAM WITH CORROSION. REPLACED FLOOR BEAM P/N: D5311281820401 BETWEEN FR12 AND FR24, Y254 IAW A319 SRM 53-11-14-08
- [SDR DALA2026052703185](https://openairdocs.org/sdr/DALA2026052703185.md): Seat Track · corroded · May 25, 2026 · N368NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > PAX CABIN AFT SECTION FLOOR STRUCTURE, BETWEEN FR64 AND FR66 AT Y-765 SEAT TRACK WITH CORROSION IN SEVERAL PLACES. C/A: REPLACED SEAT TRACK AT PAX CABIN BETWEEN FR64 AND FR66, Y-765 IAW ER/A #633966-14 REV ORIGINAL DATED 19/MAY/26, NAT DWG #14N00031 REV E AND
- [SDR DALA2026052703184](https://openairdocs.org/sdr/DALA2026052703184.md): Flap Track · excess play · May 25, 2026 · N368NB · Airbus A319114 · Trailing Edge Flaps
  > LEVEL 2 CORROSION, LH WING I/B FLAP TRACK NR 2 SUPPORT ECCENTRICAL BEARING WITH PLAY. REPAIRED LT WING I/B FLAP TRACK NR 2 SUPPORT I/B AND OTBD FITTING FACES AND AL BORE HOLES IAW DELTA ERA 633957-14 REV ORIGINAL APPROVED DATE 19/MAY/26. THIS REPAIR APPROVAL
- [SDR DALA2026052703180](https://openairdocs.org/sdr/DALA2026052703180.md): Fitting · not reported · May 22, 2026 · N368NB · Airbus A319114 · Fuselage Main, Structure
  > DAMAGE TOLERANCE EVALUATION ( DTE) REQUIRED FOR REPAIR INSTALLE D PER ER/A 633743-14AD FOR MIRROR FITTING INSTALLATION AND CONTI NUITY FITTING REPLACEMENT. SECTION I IS LIMITED TO 60000FC FROM SECTION I. ER/A TO BE REVIS ED PRIOR TO THIS LIMIT ELSE REMOVE A/C
- [SDR DALA2026052703179](https://openairdocs.org/sdr/DALA2026052703179.md): Fitting · not reported · May 22, 2026 · N368NB · Airbus A319114 · Fuselage Main, Structure
  > DAMAGE TOLERANCE EVALUATION ( DTE) REQUIRED FOR MIRROR FITTING REPAIR AND CONTINUITY FITTING REPLACEMENT PER ER/A 633743-14AD. C/A: SECTION I IS LIMITED TO 29500FC FROM SECTION I. ER/A TO BE REVIS ED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATE
- [SDR DALA2026052703178](https://openairdocs.org/sdr/DALA2026052703178.md): Fitting · not reported · May 22, 2026 · N368NB · Airbus A319114 · Fuselage Main, Structure
  > ER/A 633743-14AD ISSUED FOR CONTINUITY FITTING REPLACEMENT AND MIRROR FITTING REPAIR. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN 27000FC FROM SECTION I AND EVERY 4700F C THEREAFTER. ASSOCIATED ER/A 14-633743 ADDED FOR AC 3168. (LP: 1607258) AIRCRA
- [SDR DALA2026052403131](https://openairdocs.org/sdr/DALA2026052403131.md): Rib · corroded · May 21, 2026 · N368NB · Airbus A319114 · Wing, Rib/Bulkhead
  > LEVEL 2 CORROSION, LT WING, TRAILING EDGE REAR SPAR RIBLET WITH CORROSION AT RIB 19. PERFORMED REPLACEMENT REPAIR AT RIBLET M LOCATED AT LT WING TRAILING EDGE REAR SPAR AREA AT RIB 19 IAW SRM 57-51-12-300 -007 PARG 2.B REV 157. THIS TASK IS CATEGORY A WITH N
- [SDR DALA2026052703188](https://openairdocs.org/sdr/DALA2026052703188.md): Rib · not reported · May 19, 2026 · N368NB · Airbus A319114 · Trailing Edge Flaps
  > DAMAGE TOLERANCE EVALUATION ( DTE) REQUIRED FOR REPAIR PERFORME D ON LT INBD FLAP RIB 9 LUG PER ER/A 633957-14. SECTION I IS LIMITED TO 6 MONTHS ( 182 DAYS) FROM 15MAY26. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 1
- [SDR DALA2026051302981](https://openairdocs.org/sdr/DALA2026051302981.md): Floor Support · corroded · May 12, 2026 · N368NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, A319 TASK 5320-6010, CPCP 2021-2001. PAX CABIN, AFT SECTION, FLOOR STRUCTURE AT FR68 Y-765MM, LONGITUDINAL BEAM WITH CORROSION. C/A: REPLACED LONGITUDINAL BEAM P/N: D5347219320000 IAW A319 SRM 51- 72-11-911-001 REV 157.00 DATED 15/PR/26. (LP
- [SDR DALA2026051302979](https://openairdocs.org/sdr/DALA2026051302979.md): Skin · debonded · May 11, 2026 · N368NB · Airbus A319114 · Rudder, Plate/Skin
  > EMPENNAGE, RUDDER RH SIDE PANEL WITH DISBONDING DUE TO FLUID INGRESS WITH AN AREA OF 2073MM2 AT HOISTING POINT #3 RHS. C/A: REPAIRED RUDDER S/N TS-3438 HOIST POINTS #3 R/H SIDE AND #1 L/H SIDE I.A.W A319 SRM TASK 55-41-13-300-032 REV 157.00 DATED 15/ APR/26 (
- [SDR DALA2026051102931](https://openairdocs.org/sdr/DALA2026051102931.md): Floor Support · corroded · May 9, 2026 · N368NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORRSION, A319 TASK 5320-6010, CPCP 2021-2001. PAX CABIN AFT SECTION, FLOOR STRUCTURE BETWEEN FR66+120MM AND FR68 AT Y1292 AND Y1162.5 LONGITUDINAL BEAM (2EA SECTIONS) WITH CORROSION IN SEVERAL PLACES. REPLACED LONGITUDINAL BEAMS (2EA) P/N: D534 72172
- [SDR DALA2026050602890](https://openairdocs.org/sdr/DALA2026050602890.md): Fitting · corroded · May 5, 2026 · N368NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > LEVEL 2 CORROSION. ENGINE NR 1 PYLON AREA SPIGOT RECEPTACLE FITTING BORE WITH CORROSION AND BALL JOINT WITH INUSUAL WEAR. REPLACED NR 1 PYLON SPIGOT BALL JOINT AND FITTING IAW SRM 54-51-12-300-001, REV 157, AND AMM 54-51 -41-400-001-A, AND 54-51-41-400-001-A
- [SDR DALA2026050502831](https://openairdocs.org/sdr/DALA2026050502831.md): Shaft · not reported · May 4, 2026 · N368NB · Airbus A319114 · Trailing Edge Flaps
  > RIGHT WING REMOVE AND INSTALL TORQUE SHAFT 6282CM TO PERFORM REPAIR T/E OVERHANG AREA.: REMOVED AND REINSTALLED RT WING FLAP TORQUE SHAFT 6282CM IAW AMM TASK 27-54-45-000-013-A AND 27-54-45-400-013-A REV 135.00. (LP: 1577369)
- [SDR DALA2026050502830](https://openairdocs.org/sdr/DALA2026050502830.md): Floor Support · corroded · May 4, 2026 · N368NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, TASK 5320-6010, PAX CABIN, AFT SECTION, FLOOR STRUCTURE AT FR70 Y-464.8MM, LONGITUDINAL BEAM WITH CORROSION. REPLACED NEW BEAM P/N: D5347219520200 IAW A319 SRM 53-41-14-03A, FIG 303 SHEET 2, ITEM 155. REV 157.00, AND INATALLED IAW DWG # D
- [SDR DALA2026050502829](https://openairdocs.org/sdr/DALA2026050502829.md): Floor Support · corroded · May 4, 2026 · N368NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, TASK 5320-6010. PAX CABIN, AFT SECTION, FLOOR STRUCTURE, BETWEEN FR67 AND FR68, Y-1292 AND Y-1162.5 LONGITUDINAL BEAM (2EA SECTIONS) WITH CORROSION. REPLACED LONGITUDINAL BEAM (2EA) LOCATED AT PAX CABIN, AFT SECTION BETWEEN FR66 AND FR69, Y
- [SDR DALA2026042902698](https://openairdocs.org/sdr/DALA2026042902698.md): Shear Plate · corroded · Apr 28, 2026 · N368NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > PAX CABIN, AFT SECTION, FLOOR BTWN FR 69 & FR 70, Y-1194.8, SHEAR PLATE CORRODED. REPLACED THE SHEAR PLATE IAW SRM 53-41-17-01A, FIGURE 001, ITEM 310. REV 157. AND INSTALLED IAW DWG D534 74180, SHEET 6, ITEM 74. (LP: 1567232). AIRCRAFT WAS GROUNDED.
- [SDR DALA2026042502621](https://openairdocs.org/sdr/DALA2026042502621.md): Floor Support · corroded · Apr 24, 2026 · N368NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > TASK 5320-6010, CPCP 2021-2001. PAX CABIN AFT SECTION, FLOOR STRUCTURE AT FR68 Y512.5 LONGITUDINAL BEAM WITH CORROSION. REPLACED FLOOR STRUCTURE LONGITUDINAL BEAM P/N: 5347219420400 AT FR67 TO FR70, Y512.5 IAW A319 SRM 53-41-14-03A FIG 303, ITEM 180. REV 157.
- [SDR DALA2026031401776](https://openairdocs.org/sdr/DALA2026031401776.md): Unknown · odor · Mar 14, 2026 · N368NB · Airbus A319114 · Air Distribution System
  > AFT FA REPORTED SUSPICIONS SMELL COMING FROM GASPER CENT JUST ABOVE COFFEE MAKERS. INSP AFT GALLEY AREA, NO ABNORMAL ODOR PRESENT RAN ENGINES ISOLATED BOTH PACKS, ENG AND APU BLEED SOURCES, NO ODORS NOTED. REF W/C 0550-2002, TYPE 9. A/C OK TO CONTINUE. (LP:
- [SDR DALA2026022601354](https://openairdocs.org/sdr/DALA2026022601354.md): Proximity Sensor · out of tolerance · Feb 11, 2026 · N368NB · Airbus A319114 · Landing Gear Position and Warning
  > AFTER TAKE OFF FROM KDTW, AFTER MLG LEVER SELECTED UP, DOORS SEQUENCED TO OPEN, BUT MLG DID NOT RETRACT. MLG NOT UPLOCKED ECAM APPEARED, FOLLOWED BY ANTI ICE STBY PITOT. SELECTED GEAR DOWN, ECAM CLEARED. ELECTED GEAR UP, GEAR CYCLED NORMALLY WITH WHEEL PAGE IN
- [SDR DALA2026011700391](https://openairdocs.org/sdr/DALA2026011700391.md): Latch · broken · Jan 13, 2026 · N368NB · Airbus A319114 · Passenger Oxygen System
  > O2 MASK LATCH 27DEF BROKEN AND 26DEF BROKEN. FWD TO MEL 35- 21-01A (M) PROC C/W. PLACARD INSTALLED. WAS ABLE TO RESET O2 MASK PSU PANEL PER A319 AMM 35-21. OK FOR SVC. PLACARDS REMOVED. OK FOR SVC. (LP: 8008578)
- [SDR DALA2025073105748](https://openairdocs.org/sdr/DALA2025073105748.md): Ecs · odor · Jul 30, 2025 · N368NB · Airbus A319114 · Air Distribution System
  > ODOR AND FUME DETECTED IN FLT DECK. PERFORMED W/C 0550-2001, 0550-2002 & 2100-2005. AFTER ECS DECONTAMINATION REVERSE DUCT BURN PROCEDURE. NO FURTHER SMELLS NOTED IN FLIGHT DECK OR CABIN.
- [SDR DALA2025071505314](https://openairdocs.org/sdr/DALA2025071505314.md): Oxygen Mask · no test · Jul 9, 2025 · N368NB · Airbus A319114 · Crew Oxygen System
  > SHIP 3168 O2 MASK WILL NOT SOUND DURING TEST. CORRECTIVE ACITON: R/R OBSERVER SEAT O2 STOWAGE BOX IAW A-319 AMM 35-12. (7454926).
- [SDR DALA2025070204960](https://openairdocs.org/sdr/DALA2025070204960.md): Oxygen Box · no test · Jul 2, 2025 · N368NB · Airbus A319114 · Passenger Oxygen System
  > SHIP 3168 02 MANUAL 02 MASK DEPLOYMENT PSU ROW 24DEF RT DID NOT OPEN. CORRECTIVE ACTION: R/R PSU/O2 PANEL AT ROW 24DEF PER A319 AMM 25-25. (7194995).
- [SDR DALA2025030301593](https://openairdocs.org/sdr/DALA2025030301593.md): Bracket · damaged · Mar 1, 2025 · N368NB · Airbus A319114 · Emergency Lighting
  > SHIP 3168 DISC: AFT GALLEY EMERGENCY LIGHT BRACKET DAMAGE. C/A: REMOVED + REPLACED AFT GALLEY EMER LIGHT + BRACKET ASSY AS PER A320F AMM 25-65-01. (LP: 7087320)
- [SDR DALA2025012900688](https://openairdocs.org/sdr/DALA2025012900688.md): Light · inoperative · Jan 29, 2025 · N368NB · Airbus A319114 · Emergency Lighting
  > SHIP 3168 ROW 29 EMERGENCY EXIT LIGHT INOP AND MISSING. CORRECTIVE ACTION: INSTALLED NEW EMERGENCY LIGHT IAW A319 IPC 33-51-09. (0784893)
- [SDR DALA2024112511198](https://openairdocs.org/sdr/DALA2024112511198.md): Oxygen Mask · unwanted deploy · Nov 24, 2024 · N368NB · Airbus A319114 · Passenger Oxygen System
  > SHIP 3168 OXYGEN PANEL MASK DEPLOYED / LOCATION:29A. CORRECTIVE ACTION: REPACKED MASKS PER A319 AMM 35-23. OK FOR SERVICE. (0675189)
- [SDR DALA2024080607796](https://openairdocs.org/sdr/DALA2024080607796.md): Pylon · nicked · Aug 5, 2024 · N368NB · Airbus A319114 · Nacelle/Pylon, Attach Fittings
  > SHIP 3168 FWD ENGINE MOUNT ON PYLON, FWD ALIGNMENT PIN HOLE HAS NICK AT LOWER SURFACE MARKED. CORRECTIVE ACTION: BLENDED FWD ENG. MOUNT PYLON, FWD ALIGNMENT PIN HOLE PER A319 SRM 54-51-18. (0486691)
- [SDR DALA2024060505801](https://openairdocs.org/sdr/DALA2024060505801.md): Switch · malfunctioned · Jun 4, 2024 · N368NB · Airbus A319114 · Emergency Lighting
  > SHIP 3168 UNABLE TO TURN EMERGENCY LIGHTS OFF. CORRECTIVE ACTION: CYCLED EMERGENCY LIGHT SWITCH IN COCKPIT PER A319 AMM 33-51. (5610512)
- [SDR DALA2024060305745](https://openairdocs.org/sdr/DALA2024060305745.md): Floor Panel · damaged · Jun 2, 2024 · N368NB · Airbus A319114 · Fuselage Floor Panel
  > SHIP 3168 FWD CARGO FLOOR PANEL DAMAGED. CORRECTIVE ACTION: R/R PANEL 131AF REF A319 AMM 53-22-14. (5610500)
- [SDR DALA2024032103583](https://openairdocs.org/sdr/DALA2024032103583.md): Indicator · unknown · Mar 20, 2024 · N368NB · Airbus A319114 · Rate of Climb Indicator
  > SHIP 3168 VERTICAL SPEED INDICATOR "JUMPING" UP & DOWN WHILE PARKED AT GATE, CAPTAIN'S & FIRST OFFICERS. CORRECTIVE ACTION: OPS TEST GOOD REF A319 AMM 34-18 CKS GOOD. AFS TEST GOOD. NO FAULTS NOTED. OK FOR SVC. (5863402)
- [SDR DALA2024022302522](https://openairdocs.org/sdr/DALA2024022302522.md): Relief Valve · faulty · Feb 23, 2024 · N368NB · Airbus A319114 · Landing Gear Brake System
  > SHIP 3168 BRAKE ACCUMULATOR PRESSURE NOT STAYING IN GREEN BAND. CORRECTIVE ACTION: R&R BRAKE MANIFOLD RELIEF VALVE PER A319 AMM 32-44. LEAK & OPS CHECK GOOD. BRAKE ACCUMULATOR PRESSURE HOLDS STEADY WITHIN LIMITS. (5602191)
- [SDR DALA2024010300087](https://openairdocs.org/sdr/DALA2024010300087.md): Unknown · unknown · Jan 2, 2024 · N368NB · Airbus A319114 · Emergency Lighting
  > SHIP 3168 EMERGENCY LIGHTS CAME ON TWICE ENROUTE IN THE ARMED POSITION. CORRECTIVE ACTION: RESET CIDS 1 & 2. PERFORMED EMER LIGHT OPS CK REF A319 AMM 33-51. (5150349)
- [SDR DALA2023120509946](https://openairdocs.org/sdr/DALA2023120509946.md): Unknown · unknown · Dec 4, 2023 · N368NB · Airbus A319114 · Emergency Lighting
  > SHIP 3168 EMERGENCY LIGHTS OVERDOORS AND WING EXITS FLASH ON AND OFF. CORRECTIVE ACTION: RESET CIDS SYSTEM 1 & 2 AND PERFORMED AN EMERGENCY LIGHT TEST IAW A319 AMM 33-51. SYSTEM OPS NORMAL. OK FOR SERVICE. (4268864)
- [SDR DALA2023100208069](https://openairdocs.org/sdr/DALA2023100208069.md): Unknown · unknown · Oct 1, 2023 · N368NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3168 EXCESSIVE PLAY BEARING ON UPPER AND LOWER CONECTION LINK AND UPPER CONNECTION NEXT TO FUSELAGE OF PASSENGER CREW DOOR 842. CORRECTIVE ACTION: REPLACED BUSHES ON UPPER CONNECTION LINK ON DOOR STRUCTURE, UPPER AND LOWER CONNECTION LINK AND SUPPORT ARM
- [SDR DALA2023100208066](https://openairdocs.org/sdr/DALA2023100208066.md): Unknown · unknown · Sep 30, 2023 · N368NB · Airbus A319114 · Emergency Lighting
  > SHIP 3168 BROKEN PASSENGER SEAT EMERGENCY LIGHT ROW 21 RH IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED PASSENGER SEAT EMERGENCY LIGHT ROW 21 RH IN PASSENGER CABIN AS PER CMM-25-22-53. (2994987)
- [SDR DALA2023100308106](https://openairdocs.org/sdr/DALA2023100308106.md): Unknown · unknown · Sep 28, 2023 · N368NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3168 CORROSION INTERCONNECTING STRUT IB FLAP ASSY. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT I/B FLAP ASSY RH WING AS PER A320 FAM AMM 27-51-44-000-001-A AND AMM 21-51-44-400-001-A. (2990699)
- [SDR DALA2023100308105](https://openairdocs.org/sdr/DALA2023100308105.md): Unknown · unknown · Sep 28, 2023 · N368NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3168 CORROSION INTERCONNECTING STRUT OB FLAP ASSY. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT O/B FLAP ASSY LH WING AS PER A320 FAM AMM 27-51-44-000-001-A AND AMM 21-51-44-400-001-A. (2990691)
- [SDR DALA2023013000732](https://openairdocs.org/sdr/DALA2023013000732.md): Unknown · odor · Jan 26, 2023 · N368NB · Airbus A319114 · Air Distribution System
  > FLIGHT ATTEN. REPORTED FUMES IN CABIN ON GROUND. PERFORMED AMDS 0550-2002 AND 2100-2003 AND AMDS 2100-2004 RAN A/ C WITH ENGINES AND RAN PACK, NO SMELL NOTE NOTIFIED MCC A/C OK FOR SERVICE. (9386337)
- [SDR DALA2022122808431](https://openairdocs.org/sdr/DALA2022122808431.md): Unknown · odor · Dec 23, 2022 · N368NB · Airbus A319114 · Air Distribution System
  > MOMENTARY SWEET SMELL ON ENGINE START. PERFROM PACK BURN OUT AND REPLACE RECIRC FILTERS.
- [SDR DALA2021072804252](https://openairdocs.org/sdr/DALA2021072804252.md): Oil System · leaking · Jul 25, 2021 · N368NB · Airbus A319114 · APU Oil System
  > SHIP 3168 - SMKE/FUME, ON GROUND RUNNING APU, CABIN FILLED WITH LIGHT BLUE SMOKE & SMELLED LIKE STICKY SOCK ODOR. MTC FOUND APU COMPARTMENT SOAKED IN OIL. APU PLACED ON MEL AND ECS DECONTAMINATION PROCEDURE COMPLETED. NO FURTHER SMOKE OR SMELL. A/C RTS.(7928
- [SDR DALA2021061003172](https://openairdocs.org/sdr/DALA2021061003172.md): Panel · damaged · Jun 8, 2021 · N368NB · Airbus A319114 · Passenger Oxygen System
  > SHIP 3168 - DURING W/C 2527, FOUND FWD LAV L1 O2 PANEL WILL NOT STOW. CORRECTIVE ACTION: REPLACED OXYGEN CONTAINER PANEL UNIT AT FWD LAV L1 201 PER A319 AMM 35-21-41 AND 25-25-43.OPERATIONAL CHECK SATISFACTORY. (7315702)
- [SDR DALA2021061003171](https://openairdocs.org/sdr/DALA2021061003171.md): Psu · no test · Jun 8, 2021 · N368NB · Airbus A319114 · Emergency Equipment
  > SHIP 3168 - DURING W/C 2527 O2 PSU AT ROW 21A FAILED TO DROP. CORRECTIVE ACTION: REPLACED OXYGEN CONTAINER PANEL UNIT AT SEAT ROW 21ABC PER A319 AMM 35-21. OPERATIONAL CHECK SATISFACTORY PER A319 AMM 35-23-00. (7315701)
- [SDR DALA2021061003170](https://openairdocs.org/sdr/DALA2021061003170.md): Psu · no test · Jun 8, 2021 · N368NB · Airbus A319114 · Emergency Equipment
  > SHIP 3168 - DURING W/C 2527 O2 PSU ABOVE L1 DOOR FAILED TO DROP. CORRECTIVE ACTION: REMOVED & REPLACED L1 DOOR O2 GENERATOR & CONTAINER REF A319 AMM 35-21. OPS CHECK GOOD. (7315700)
- [SDR DALA2021042702437](https://openairdocs.org/sdr/DALA2021042702437.md): Line · leaking · Apr 25, 2021 · N368NB · Airbus A319114 · Hydraulic System, Main
  > SHIP 3168. HYD. ENROUTE TO GDL, GREEN RSVR LO LVL ECAM MESSAGE, QRH REQUIRED GRAVITY GEAR EXTENSION. CORRECTIVE ACTION: FOUND RT WING SPOILER ACTUATOR LEAKING FROM SERVO VALVE GASKET AND O RINGS. REPLACED AND RETURNED TO SERVICE. (7653134)
- [SDR DALA2021010400034](https://openairdocs.org/sdr/DALA2021010400034.md): Clamp · leaking · Jan 4, 2021 · N368NB · Airbus A319114 · Pneumatic Distribution System
  > DIV TO RIC DUE TO RT WING AIR LEAK MESSAGE. CORRECTIVE ACTION: FOUND PNEUMATIC CROSS-BLEED VALVE CLAMPS LEAKING. REPLACED CLAMPS AND RETURNED TO SERVICE.
- [SDR DALA2020102203423](https://openairdocs.org/sdr/DALA2020102203423.md): Power Supply · inoperative · Oct 17, 2020 · N368NB · Airbus A319114 · Emergency Lighting
  > INOPERABLE EPSU-EMERGENCY POWER SUPPLY UNIT 11WL IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT 11WL IN PASSENGER CABIN, AS PER A320 FAM AMM 33-51-38-000-A AND AS PER A320 FAM AMM 33-51.
- [SDR DALA2020110603616](https://openairdocs.org/sdr/DALA2020110603616.md): Fuel Tank · corroded · Oct 16, 2020 · N368NB · Airbus A319114 · Fuel Storage
  > CORROSION EXTERNAL SKIN ON CENTER TANK LOCATED BETWEEN FR 41 TO FR 42 AND BETWEEN Y1732 TO Y1292 IN PASSENGER CABIN. CORRECTIVE ACTION: EVALUATED REWORK LOCATED ON EXTERNAL SKIN ON CENTER TANK LOCATED BETWEEN FR 41 TO FR 42 AND BETWEEN Y1732 TO Y1292 IN PASSE
- [SDR DALA2020102303449](https://openairdocs.org/sdr/DALA2020102303449.md): Skin · damaged · Oct 16, 2020 · N368NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOWER TAIL SECTION LOCATED BETWEEN FR 70 TO FR 77 FROM STR 20R TO STR 20L LOWER FUSELAGE. CORRECTIVE ACTION: LOWER TAIL SECTION LOCATED BETWEEN FR 70 TO FR 77 FROM STR 20R TO STR 20L LOWER FUSELAGE (
- [SDR DALA2020102203420](https://openairdocs.org/sdr/DALA2020102203420.md): Stringer · corroded · Oct 16, 2020 · N368NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 44 LOCATED AT FR 65 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON STRINGER 44 LOCATED AT FR 65 IN AFT CARGO COMPARTMENT, AS PER ER/A 588013-14 REV. ORIGINAL AND PRI 588013-14 REV 0.

Next page: https://openairdocs.org/aircraft/N368NB/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N368NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N368NB/reports

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